NTSB MIA93LA042 — 1993-01-01 · TITUSVILLE, Florida, United States

Current FAA registration · N82542

Make / Model: PIPER PA-32R-301
Engine: LYCOMING IO-540 SER (300 hp)
Seats / Engines: 7 seats · 1 engine
Last airworthiness date: 19820914
ADS-B equipped: Yes — Mode-S AB466D

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

N82542 Piper PA-32R-301 Minor

Probable cause & findings

LOSS OF ENGINE POWER DURING THE DOWNWIND LEG FOR UNDETERMINED REASONS, POOR IN-FLIGHT PLANNING/DECISION BY THE DUAL STUDENT, AND INADEQUATE SUPERVISION BY THE PILOT-IN-COMMAND (CFI).

Factual narrative

AFTER TAKEOFF FOLLOWING THE THIRD TOUCH & GO LANDING ON RWY 36, DURING THE DOWNWIND LEG WHERE THE FLT WAS ABOUT 1 MILE WEST OF THE DEPARTURE RWY, THE STUDENT ADVISED THE CFI THAT HE SMELLED SOMETHING BURNING & THAT THE ENG WASN'T PRODUCING POWER. THE CFI ADVANCED & RETARDED THE THROTTLE & OBSERVED THAT THE MANIFOLD PRESSURE NEEDLE MOVEMENT FOLLOWED THE THROTTLE MOVEMENT, THEN GAVE CONTROL OF THE ACFT BACK TO THE STUDENT. THE STUDENT AGAIN STATED THAT THE ENG WASN'T PRODUCING POWER & THE CFI TOOK CONTROL, TURNED TO THE EAST TO LAND ON A TAXIWAY, & LANDED HARD SHORT OF THE TAXIWAY. FUEL QUANTITY WAS SUFFICIENT TO SUSTAIN ENG OPERATION & THE FUEL SUPPLY DID NOT CONTAIN CONTAMINANTS. THE ENG WAS STARTED AFTER THE ACCIDENT & OPERATED ONLY TO 1,500 RPM DUE TO DAMAGE TO THE PROPELLER ASSY. THE ENG WAS THEN SENT TO THE MANUFACTURER'S FACILITY OPERATED WITH THE ONLY DISCREPANCY NOTED THAT THE FUEL FLOW AT 80 PPH WAS 9 PPH LEANER THAN SPECIFICATION. NO DETERMINATION COULD BE MADE AS TO THE REASON FOR THE LOSS OF ENG POWER. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1993_MIA93LA042.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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